Page 123 - 《真空与低温》2025年第4期
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538                                         真空与低温                                   第 31 卷 第  4  期


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                  ence,Boston,Massachusetts,June,2022.               ion engine plume characteristics[C]//30  Joint Propulsion
              [366]   LAFLEUR T,RAFALSKYI D,AANESLAND A. Radio-      Conference  and  Exhibit, Indianapolis, IN, USA, AIAA,
                                                  th
                  frequency biasing of ion thruster grids[C]//36  International  1994.
                  Electric Propulsion Conference,University of Vienna,Aus-  [378]   PATTERSON M J,ROMAN R F,FOSTER J E. Ion en-
                  tria,September 15-20,2019.                         gine  development  for  interstellar  precursor  missions[C]//
                                                                      th
              [367]   RAFALSKYI D,AANESLAND A. A neutralizer-free gri-  36  AIAA/ASME/SAE/ASEE Joint Propulsion Conference
                  dded ion thruster embedded into a 1U cubesat module[C]//  and Exhibit,24-28 July,Las Vegas,NV,USA ,2000.
                  35  International Electric Propulsion Conference,Atlanta,  [379]   RAWLIN V K. Status of ion engine development for high
                    th
                                                                                                    th
                  Georgia,October,2017.                              power,high specific impulse missions[C]//27  International
              [368]   AANESLAND A,POPELIER L,LERAY G. Plasma pro-    Electric Propulsion Conference,Pasadena,California,USA,
                                                st
                  pulsion with electronegative gases[C]//31  International El-  October,2001.
                  ectric Propulsion Conference,Ann Arbor,MI,USA,Septe-  [380]   FOSTER J E,PATTERSON M J. Discharge characteriza-
                  mber,2009.                                         tion of 40 cm-microwave ECR ion source and neutralizer
                                                                          th
              [369]   GARRIGUES L,HAGELAAR G J M,LEVKO D. Two-       [C]//39  Joint Propulsion Conference and Exhibit cospon-
                  dimensional particle-in-cell model of the extraction region  sored by the AIAA,ASME,SAE,and ASEE Huntsville,
                                                     rd
                  of  the  PEGASES  ion-ion  plasma  source[C]//33   Interna-  Alabama,July 20-23,2003.
                  tional  Electric  Propulsion  Conference, Washington, DC,  [381]   MECKEL N,POLAHA J. Structural analysis of pyrolytic
                                                                                                        th
                  USA,October,2013.                                  graphite optics for the HiPEP ion thruster[C]//40  AIAA/
              [370]   LAFLEUR  T  A.  Proof-of-concept  demonstration  of  the  ASME/SAE/ASEE Joint Propulsion Conference and Exhi-
                                           th
                  PEGASES  plasma  thruster[C]//34   International  Electric  bit,11-14 July,2004,Fort Lauderdale,Florida,2004.
                  Propulsion Conference and 6th Nano-satellite Symosium,  [382]   PATTERSON M J,HERMAN D,SHASTRY R. Annular-
                  Hyogo-Kobe,Japan,July 4-10,2015.                   geometry ion engine:concept,development status,and pre-
                                                                                          th
              [371]   MAZOUFFREA S,RENAUD D. A new ion–ion plasma    liminary  performance[C]//48   AIAA/ASME/SAE/ASEE
                  thruster with an annular geometry[J]. The European Physi-  Joint Propulsion Conference and Exhibit,Atlanta,Georgia,
                  cal Journal D,2017,71:298.                         AIAA,2012.
              [372]   KODA D,KUNIN H. Ion engine combining positive and  [383]   SHASTRY R,PATTERSON M J,HERMAN D A. Current
                                 th
                  negative ions[C]//34  International Electric Propulsion Con-  density measurements of an annular-geometry ion engine
                                                                          th
                  ference  and  6th  Nano-satellite  Symosium, Hyogo-Kobe,  [C]//48  AIAA/ASME/SAE/ASEE Joint Propulsion Confe-
                  Japan,July 4-10,2015.                              rence and Exhibit,Atlanta,Georgia,AIAA,2012.
              [373]   HOFFMANL D,GRUBISIC A. Discharge-mode testing of  [384]   PATTERSON M J. Annular engine development status[C]//
                                                                      th
                  the  X-EPT  microwave  ECR  gridded  ion  thruster[C]//25 th  48  AIAA/ASME/SAE/ASEE Joint Propulsion Conference
                  International Electric Propulsion Conference,Vienna,Aus-  and Exhibit,San Jose,CA,AIAA,2013.
                  tria,September,2019.                          [385]   PATTERSON M J. Annular ion engine:evolutionary ap-
              [374]   FARNELL C C,THOMPSON S J,WILLIAMS J D. Ad-     proach to achieve revolutionary capabilities[C]//Space Tech
                                                  th
                  ditive  manufacturing  for  ion  optics[C]//37   International  Conference,Pasadena,2016.
                  Electric  Propulsion  Conference, Boston, Massachusetts,  [386]   王彦龙,杨浩,李兴达,等. 5 kW  环型离子推力器试验研
                  June,2022.                                         究  [J]. 深空探测学报(中英文),2017,4(3):232−237.
              [375]   BROPHY J R. Near-term,100 kW class ion engines[C]//  [387]   CHEN J J,ZHANG T P,LIU M Z. Modeling and simula-
                  Conference on Advanced SEI Technologies 4-6 September,  tion of the effect of cathode gas flow on the lifetime and
                  1991.                                              performance of an annular-geometry ion engine[J]. IEEE
              [376]   BROPHY J R,MUELLER J,PLASS L C. Segmented ion  Transactions on Plasma Science,2019,47:357−364.
                                                 th
                  engine  operation  and  performance[C]//30   Joint  Propul-  [388]   CASAREGOLA  C, CESARETTI  G, ANDRENUCCI  M.
                  sion  Conference  and  Exhibi, Indianapolis, USA, AIAA,  HiPER:A European programme to develop electric propul-
                  1994.                                              sion  technologies  for  future  space  exploration[C]//Space
              [377]   TIERNCY C M,BROPHY J R,MUELLER J. Segmented    Propulsion 2010,San Sebastian,Spain,2010.
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